EP2885356A1 - Method for producing an escape route marking for air planes, and said escape route marking - Google Patents
Method for producing an escape route marking for air planes, and said escape route markingInfo
- Publication number
- EP2885356A1 EP2885356A1 EP13756310.2A EP13756310A EP2885356A1 EP 2885356 A1 EP2885356 A1 EP 2885356A1 EP 13756310 A EP13756310 A EP 13756310A EP 2885356 A1 EP2885356 A1 EP 2885356A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- escape route
- support
- carrier element
- translucent cover
- route marking
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 13
- 239000000463 material Substances 0.000 claims abstract description 39
- 238000000034 method Methods 0.000 claims abstract description 28
- 238000010438 heat treatment Methods 0.000 claims abstract description 5
- 238000007711 solidification Methods 0.000 claims description 26
- 230000008023 solidification Effects 0.000 claims description 26
- 239000003550 marker Substances 0.000 claims description 22
- 239000004417 polycarbonate Substances 0.000 claims description 20
- 229920000515 polycarbonate Polymers 0.000 claims description 20
- 239000000049 pigment Substances 0.000 claims description 11
- 229920001296 polysiloxane Polymers 0.000 claims description 10
- 239000004033 plastic Substances 0.000 claims description 6
- 229920003023 plastic Polymers 0.000 claims description 6
- 238000004040 coloring Methods 0.000 claims description 2
- 230000009477 glass transition Effects 0.000 description 7
- 239000011159 matrix material Substances 0.000 description 5
- 238000002844 melting Methods 0.000 description 5
- 230000008018 melting Effects 0.000 description 5
- 229920000642 polymer Polymers 0.000 description 3
- 238000001816 cooling Methods 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 239000007791 liquid phase Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000012071 phase Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000012790 confirmation Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 238000005424 photoluminescence Methods 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21K—NON-ELECTRIC LIGHT SOURCES USING LUMINESCENCE; LIGHT SOURCES USING ELECTROCHEMILUMINESCENCE; LIGHT SOURCES USING CHARGES OF COMBUSTIBLE MATERIAL; LIGHT SOURCES USING SEMICONDUCTOR DEVICES AS LIGHT-GENERATING ELEMENTS; LIGHT SOURCES NOT OTHERWISE PROVIDED FOR
- F21K2/00—Non-electric light sources using luminescence; Light sources using electrochemiluminescence
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C51/00—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
- B29C51/002—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor characterised by the choice of material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C51/00—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
- B29C51/12—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor of articles having inserts or reinforcements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C51/00—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
- B29C51/26—Component parts, details or accessories; Auxiliary operations
- B29C51/30—Moulds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60Q—ARRANGEMENT OF SIGNALLING OR LIGHTING DEVICES, THE MOUNTING OR SUPPORTING THEREOF OR CIRCUITS THEREFOR, FOR VEHICLES IN GENERAL
- B60Q3/00—Arrangement of lighting devices for vehicle interiors; Lighting devices specially adapted for vehicle interiors
- B60Q3/40—Arrangement of lighting devices for vehicle interiors; Lighting devices specially adapted for vehicle interiors specially adapted for specific vehicle types
- B60Q3/41—Arrangement of lighting devices for vehicle interiors; Lighting devices specially adapted for vehicle interiors specially adapted for specific vehicle types for mass transit vehicles, e.g. buses
- B60Q3/46—Emergency lighting, e.g. for escape routes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60Q—ARRANGEMENT OF SIGNALLING OR LIGHTING DEVICES, THE MOUNTING OR SUPPORTING THEREOF OR CIRCUITS THEREFOR, FOR VEHICLES IN GENERAL
- B60Q3/00—Arrangement of lighting devices for vehicle interiors; Lighting devices specially adapted for vehicle interiors
- B60Q3/70—Arrangement of lighting devices for vehicle interiors; Lighting devices specially adapted for vehicle interiors characterised by the purpose
- B60Q3/78—Arrangement of lighting devices for vehicle interiors; Lighting devices specially adapted for vehicle interiors characterised by the purpose for generating luminous strips, e.g. for marking trim component edges
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
- C09D5/00—Coating compositions, e.g. paints, varnishes or lacquers, characterised by their physical nature or the effects produced; Filling pastes
- C09D5/22—Luminous paints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2069/00—Use of PC, i.e. polycarbonates or derivatives thereof, as moulding material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2883/00—Use of polymers having silicon, with or without sulfur, nitrogen, oxygen, or carbon only, in the main chain, as mould material
- B29K2883/005—LSR, i.e. liquid silicone rubbers, or derivatives thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0018—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular optical properties, e.g. fluorescent or phosphorescent
- B29K2995/0035—Fluorescent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2009/00—Layered products
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/772—Articles characterised by their shape and not otherwise provided for
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21W—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS
- F21W2107/00—Use or application of lighting devices on or in particular types of vehicles
- F21W2107/30—Use or application of lighting devices on or in particular types of vehicles for aircraft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21W—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS
- F21W2111/00—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00
Definitions
- the present invention relates to a method for producing an escape route marking for aircraft and to an escape route marking produced by the method.
- Escape route markings are of particular importance in emergency situations where the power supply can not always be guaranteed. It is known for escape route marking in aircraft, which is also referred to as emergency marking to arrange photoluminescent strips on the floor in the interior of the aircraft. Photoluminescence is sometimes referred to as afterglow and / or phosphorizing. The safety requirements are specified, for example, in the German industrial standard DIN 67 510. The strips are laid in a straight line on the floor and, in an emergency, direct the passengers and the crew to the exits and emergency exits. In the past, photoluminescent strips have increasingly prevailed in the design of aircraft, since they are fail-safe and can be operated without a power supply.
- an emergency lighting in which a photoluminescent strip is arranged in a transparent support member.
- the carrier element can be formed in one, two or three pieces.
- Each support member has an elongate rectangular shape and accordingly can be laid in a 90 ° and 180 ° orientation to another support member.
- EP 0 489 561 A1 discloses a permanently fluorescent layer in which color pigments are incorporated into a polymer matrix.
- the fluorescent material may be incorporated in a carrier which imparts different optical properties to the fluorescent light through additional filters.
- FR 2 308 155 A1 discloses security signs deposited with photoluminescent material.
- US 4,208,300 describes a composition for photoluminescent material that can be used on stairways and on the road.
- EP 08 28 657 B2 describes an escape route marking which has two thin layers of photoluminescent material in order to increase the light emission.
- the light transmission through the photoluminescent material is through a printed or colored patchy translucent cover or modified by a color filter below the cover.
- the object is achieved by a method for producing an escape route marking according to claim 1 and an escape route marking produced by the method according to the invention according to claim 11.
- Advantageous embodiments each form the subject of the dependent claims.
- the method according to the invention for producing an escape route marking provides for the use of a heatable and deformable support form.
- the manufacturing process comprises the following steps: The heatable and deformable support form is provided so that a support member can be introduced into the support mold. A photoluminescent material and a translucent cover are placed on the support member in the support mold. After arranging the escape route marking with its various layers in the support form, the support mold is heated together with the escape route marking and preferably subsequently deformed to the heating. In the deformed position, the escape route marker solidifies in the support form.
- an escape route marking produced by the method according to the invention can be laid on the floor of an aircraft and / or along the contours of the furniture in the aircraft.
- the escape route marker's photoluminescent material shows passengers and crew the shortest route to an emergency exit in an emergency.
- the escape route markings can also be better integrated into the aesthetics of the interior of the aircraft, without affecting the safety requirements.
- the photoluminescent material and the translucent cover are arranged one above the other in the support form on the support element or these are already arranged one above the other in the support form.
- Particularly preferred support forms are used, which are made of silicone, wherein after solidification in the support form, the support form in their non-deformed Initial position returns and the escape route marker remains in its deformed position.
- Silicone molds are particularly resistant, as well as flexibly deformable and at the same time sufficiently robust. Furthermore, adhesion of the layers arranged on one another to the silicone mold is prevented due to the properties of the silicone. Due to the fact that the support form returns to its undeformed starting position after solidification, the support form can be reused for the production of further escape route markings, as a result of which such a support form can be used economically.
- the escape route marking in the support form is first heated in the support mold and arranged for deformation and / or solidification in a solidification device.
- the solidification device is provided to support the support form and allows to let the superimposed parts in the support form evenly frozen cool.
- the solidification device is provided as a prefabricated solidification mold.
- the preformed solidification mold is more stable and substantially non-deformable compared to the support mold.
- a low elasticity of the solidification mold is advantageous for placing the heated support mold in the solidification mold.
- the solidification device is designed as a forming device with a control unit.
- a formed with a control unit forming device is preferably programmable, whereby any deformations can be adjusted via the control unit.
- the transformation device has a plurality of parallel arranged rods, which are displaceable by the control unit along its longitudinal direction, to bring the escape route marking in the predetermined position.
- the use of a plurality of rods arranged in parallel makes it possible to bring about individual deformations of the support form and the escape route marking arranged therein.
- the insertion of the support form in the forming device is substantially simplified by the rods are first moved back along its longitudinal direction via the control unit, so that the support mold is convenient to use.
- the rods are moved into the specific position forming the deformation only after the onset of the heated support form, so that the heated support form including the escape route marking arranged therein can cool down and the latter solidify.
- the rods of the forming device can be transferred from its deformation position to a position that allows to easily remove the support form and the solidified in the support form escape route marker from the forming device.
- the translucent cover comprises a thermally deformable plastic, preferably polycarbonate.
- Polycarbonates are plastics which have both a glass transition temperature and a melting temperature. Below the glass transition temperature, also called softening temperature, the amorphous phase of the polycarbonate is in a solidified state, while above the glass transition temperature, the polycarbonate is in a rubber-elastic state. In the rubber-elastic state, the polycarbonate is softened and can be deformed accordingly. At temperatures above the Melting temperature, the polycarbonate is in a liquid phase in which it can be preferably mixed with color pigments or other substances. Polycarbonates and other plastics can consequently be mixed particularly well with other substances in one temperature range and thermally deformed in another temperature range.
- the carrier element and / or the photoluminescent material and / or the translucent cover are each thermally deformable alone or together.
- Thermally deformable materials are individually deformable, making them easier and better adapted to the contours of the furniture in the interior of an aircraft. If the carrier element and / or the photoluminescent material and / or the translucent cover are thermally deformed one upon the other, possible displacements of the layers with one another or with one another can be avoided.
- the escape route marking produced by the method according to the invention has a light-permeable cover and a photoluminescent material.
- Such an escape route marking can be laid on the floor and / or along the contours of the furniture in the aircraft.
- the escape route marker's photoluminescent material shows passengers and crew the shortest route to an emergency exit in an emergency.
- the translucent cover has color pigments which lead to a light-permeable coloring of the escape route marking.
- the translucent cover can be color-matched by the color pigments to the furniture in the aircraft, whereby the escape route markings can be better integrated into the aesthetics of the interior of the aircraft, without affecting the safety requirements.
- different colored differently colored pigments are used, so that the translucent covers the escape route markers can be adjusted accordingly.
- escape route markers that were color matched they could not be readily deformed, as on the luminescent strips, for example, foil strips were arranged. When deforming such a film strip, the film would be crumpled or even torn.
- the escape route marking has at least one non-linear route section with one or more radii. Escape route markings with non-linear sections can run in bends and curves. In this way, the escape route marking can be individually adapted to the configurations of the aircraft interior and thereby follow predetermined contours, in particular the Mobiliars.
- Non-linear sections are strip-shaped sections of the escape route marking referred to, which do not extend straight in the plane in which they are laid, but describe an arc.
- the escape route marking has at least one curved section with opposing curvatures.
- the escape route marking produced by the method according to the invention can be produced with opposite curvatures, in particular with left-curved and right-curved sections, whereby any curved escape route markings with smooth transitions arise. Due to the opposite curvatures, curved sections along their contour have a turning point at which a right or left curvature changes into a left or right curvature.
- the light-permeable cover has a thermally deformable plastic, preferably polycarbonate. Polycarbonates are plastics which have both a glass transition temperature and a melting temperature.
- the amorphous phase of the polycarbonate is in a solidified state, while above the glass transition temperature, the polycarbonate is in a rubber-elastic state. In the rubber-elastic state, the polycarbonate is softened and can be deformed accordingly.
- the polycarbonate is in a liquid phase in which it can preferably be mixed with color pigments. Consequently, on the one hand, polycarbonates can be dyed particularly well in one temperature range and thermally deformed in another temperature range.
- the photoluminescent material is provided in the form of strips having a length and a width corresponding to the dimensions of the translucent cover.
- the photoluminescent strips may comprise photoluminescent pigments, for example, which are incorporated in a polymer matrix, preferably in a silicone or polycarbonate matrix.
- the photoluminescent material is arranged on or in a carrier element in the form of a strip corresponding to the dimensions of the carrier element, and the light-permeable cover is arranged thereon.
- the translucent cover thus provides protection for the photoluminescent material from damage and moisture.
- a base area of the carrier element is rectangular, with side walls with a thickness D extending along each boundary of the base area at an angle to the base area, whereby a recess is formed in the carrier element.
- the side walls are perpendicular to the base. In such a recess, a photoluminescent material can be safely placed against slipping.
- the translucent cover has a rectangular base surface which has projections extending in an angle in the form of sidewalls with a thickness D 'at a distance from the boundary of the base surface, the projections being designed such that their projections Outer sides abut against the inner sides of the side walls of the support member and between the transparent cover and the support member, a cavity for receiving the photoluminescent material is formed when the translucent cover is placed on the support member.
- the translucent cover and the carrier element are formed as a one-piece hollow profile.
- a photoluminescent light strip can then be introduced into the hollow profile, preferably by injecting or pouring a silicone or polycarbonate composition in which the photoluminescent pigments are incorporated.
- FIGS. Show it: 1 is a view of a straight, colored light strip with colored cover,
- FIG. 2 is a cross-sectional view of a straight, colored light strip with a colored cover
- FIG. 3A is a cross-sectional view of a straight, colored luminous strip according to FIG. 2 in a first support form
- 3B is a cross-sectional view of a second support form
- Fig. 5 shows a forming device with a plurality of rods, wherein in the
- Forming device is a support mold is inserted and
- Fig. 6 is a plan view of an individually deformed in the plane
- Fig. 1 shows an escape route marker 1 in a straight shape with a colored translucent cover 6. Under the colored translucent cover 6 a luminescent, photoluminescent material 8 is arranged, which in turn is arranged lying flat on a support member 4.
- the photoluminescent material is provided according to FIG. 1 in a transparent carrier element.
- the support member may be transparent, but may also not be translucent, if it is connected in the installed state of the escape route marking to the ground.
- the photoluminescent material may also be cast into the transparent support member be.
- the photoluminescent material may then consist, for example, of photoluminescent pigments incorporated in a polymer matrix, preferably a silicone or polycarbonate matrix.
- FIG. 2 shows a cross-sectional view of the escape route marking according to FIG. 1. It can be seen in the cross section that the carrier element 4 has a recess 5 into which the photoluminescent material 8 is inserted. According to FIG. 2, the dimensions of the photoluminescent material 8 are slightly smaller than the recess 5 of the carrier element 4, so that laterally there is a longitudinally extending joint into which the side walls of the cover are immersed. A cover 6 is applied to the photoluminescent material 8 and terminates laterally with the edge of the carrier element 4. The joints between the edges of the photoluminescent material 8 and the edges of the recess 5 are filled with the projections of the cover 6. Alternatively, the photoluminescent material 9 can be cut to fit the recess 5 of the carrier element 4.
- the rectangular cover has no projections, but is glued or welded to the carrier element, for example.
- the gluing or welding of cover and carrier element can be carried out before or after a light strip has been arranged in the carrier element. If the luminescent strip is introduced into the hollow profile formed from cover and carrier element only after bonding or welding, this can preferably be done by introducing a silicone or polycarbonate mass containing the photoluminescent pigments.
- FIG. 3A shows the straight escape route marking from FIG. 2, inserted into a support form 2.
- the support form 2 has a cup-shaped body 2a, in which the straight escape route marking is inserted. Furthermore, the support form 2 has a Cover 2b with a stem-shaped protruding part 2c on.
- the stamp-like projection 2c makes it possible to make the surface of the escape route mark planar by the action of the weight force of the lid 2b.
- the support mold including the layers introduced is heated to a temperature.
- the support mold is heated to a temperature which is above the glass transition temperature but below the melting temperature of the materials used.
- a thermocouple can be arranged in the support form, which is arranged on or in the photoluminescent mass.
- the support mold 2 is inserted either into a prefabricated solidification mold according to FIG. 4 or into a deformation apparatus 22 according to FIG. 5.
- Fig. 3B shows an alternative embodiment of a support mold 2 '.
- the support mold 2 ' has a pot-shaped body 2a', in which the escape route marking with its support element 4, the photoluminescent material 8 and the cover 6 is arranged.
- a T-shaped punch 2c ' is arranged, which is held in the cup-shaped body 2a'.
- the T-shaped punch 2c ' has a punch head 3 and a punch stem 5.
- the punch head 3 is held in the cup-shaped body 2a'.
- the T-shaped punch 2c ' for example, by the cup-shaped body 2a' is bent and the punch is used.
- the cup-shaped body 2a ' may be formed with rounded corners E. Rounded corners prevent tearing of the support form during the bending process. It is preferred for the Support form uses a silicone with the largest possible tear and tear propagation resistance.
- the preformed solidification mold 20 shown in FIG. 4 is substantially more stable in relation to the support mold 2 and preferably permits only minimal deformation movements due to its low elasticity. Due to the minimal elasticity, the heated support mold 2 can be more easily inserted into the prefabricated solidification mold 20, so that the support mold 2 can cool with a secure grip and with uniform fixation and the introduced escape route marking 4, 6, 8 solidify and thus formed a thermally deformed escape route marker is. After solidification, the thermally deformed escape route marker 1 and the support mold 2 can be removed from the prefabricated solidification mold 20 and separated from each other. The process of cooling can also be actively supported by cooling, for example with air.
- the heated support mold 2 is inserted into the forming device 22, wherein the plurality of rods 24 are initially positioned correspondingly far apart, so that the support mold 2 can be conveniently inserted into the forming device 22.
- the rods 24 can be moved via the control unit 20 in a desired position, so that the rods 24 define a predefined deformation of the support form.
- the support mold 2 in the forming apparatus 22 may be cooled in its deformed position so that an escape route marker 1 is formed in accordance with the deformation set by the bars 24.
- the rods 24 can be moved back out of their deformation-forming position, so that the support mold 2 is conveniently removed from the forming device 22 can be. Since the support mold 2 returns to its original position, the molded escape route marker 1 can be easily removed from the support mold 2.
- the support form 2 is already used prior to its heating in the forming device 22 and only heated there before the rods 24 are moved to the desired deformation position.
- FIG. 6 shows, by way of example, the plan view of an escape route marker 1 which has been individually deformed in the plane, with the support form 2 being used for deformation in conjunction with the solidification mold 20 according to FIG. 4 or the conversion device 22 according to FIG. 5.
- the escape route marking 1 according to FIG. 6 is designed with a curved contour, wherein curved means that the contour of the escape route marking has a turning point between two opposite curvatures.
- the escape route marker 1 is therefore produced by simple means and can be produced at the same time with any shape.
- the inventive method for producing the escape route marker 1 is also implement with simple means. Further, the means used for the method of manufacture may be reused for a variety of escape route markers.
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102012016046A DE102012016046B3 (en) | 2012-08-14 | 2012-08-14 | Method for producing an escape route marking for aircraft and such |
PCT/EP2013/002444 WO2014026764A1 (en) | 2012-08-14 | 2013-08-14 | Method for producing an escape route marking for air planes, and said escape route marking |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2885356A1 true EP2885356A1 (en) | 2015-06-24 |
EP2885356B1 EP2885356B1 (en) | 2017-07-19 |
Family
ID=49111099
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13756310.2A Active EP2885356B1 (en) | 2012-08-14 | 2013-08-14 | Method for producing an escape route marking for air planes, and said escape route marking |
Country Status (5)
Country | Link |
---|---|
US (1) | US9702509B2 (en) |
EP (1) | EP2885356B1 (en) |
CN (1) | CN105051124B (en) |
DE (1) | DE102012016046B3 (en) |
WO (1) | WO2014026764A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108583464A (en) * | 2018-04-27 | 2018-09-28 | 上海应用技术大学 | A kind of automobile-used strip-type fluorescent crystal protection side and preparation method thereof |
GB201820277D0 (en) * | 2018-12-12 | 2019-01-30 | Saf T Glo Ltd | Emergency lighting system |
CZ308334B6 (en) * | 2019-07-04 | 2020-05-20 | EternaLight s.r.o. | Process for producing a photoluminescent element |
GB202117498D0 (en) * | 2021-12-03 | 2022-01-19 | Saf T Glo Ltd | Aircraft emergency way guidance assemblies |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4208300A (en) * | 1973-07-11 | 1980-06-17 | Gravisse Philippe E | Photoluminescent materials and method of manufacturing same |
FR2308155A1 (en) * | 1975-04-18 | 1976-11-12 | Aerospatiale | Photo luminescent illuminated display system - has photo luminescent source with back scattering reflector and transparent cover with opaque symbols etc. |
US4401050A (en) * | 1981-06-08 | 1983-08-30 | Britt Laurence D | Phosphorescent escape route indicator |
NL8503017A (en) * | 1985-11-04 | 1987-06-01 | Holman Associates | EMERGENCY AND / OR MARKING LIGHTS, IN PARTICULAR FOR AIRCRAFT, VESSELS AND VEHICLES, PROVIDED WITH SUCH LIGHTING FOR THE EMERGENCY LIGHTING. |
ZA918849B (en) | 1990-12-06 | 1992-08-26 | Minnesota Mining & Mfg | Articles exhibiting durable fluorescence |
US5415911A (en) * | 1992-01-16 | 1995-05-16 | Stimsonite Corporation | Photoluminescent retroreflective sheeting |
WO1996033093A1 (en) * | 1995-04-20 | 1996-10-24 | Saf-T-Glo Aerospace Limited | Emergency lighting |
EP1970101B1 (en) * | 2007-03-13 | 2011-05-18 | Lufthansa Technik AG | Escape route markings for an airplane |
EP1970100B1 (en) * | 2007-03-13 | 2012-05-16 | Lufthansa Technik AG | Escape route markings for an airplane |
GB2448424B (en) | 2007-04-14 | 2012-04-04 | Saf T Glo Ltd | Improvments in or relating to emergency lighting |
PL1987861T3 (en) * | 2007-05-04 | 2010-11-30 | Lufthansa Technik Ag | Escape route markings for an airplane |
DE102008011405A1 (en) * | 2008-02-27 | 2009-09-10 | Lufthansa Technik Ag | Escape route marking for a vehicle and method for making an escape route marking |
DE102009040040B4 (en) * | 2009-09-01 | 2012-04-19 | Lufthansa Technik Ag | Method of making an escape route marker |
DE102009040042B4 (en) | 2009-09-01 | 2013-08-29 | Lufthansa Technik Ag | Method for producing an escape route marking and one such |
KR20140007047A (en) * | 2012-07-06 | 2014-01-16 | 정영길 | Method for manufacturing the guide panel and the structure of the guide panel |
-
2012
- 2012-08-14 DE DE102012016046A patent/DE102012016046B3/en not_active Expired - Fee Related
-
2013
- 2013-08-14 EP EP13756310.2A patent/EP2885356B1/en active Active
- 2013-08-14 WO PCT/EP2013/002444 patent/WO2014026764A1/en active Application Filing
- 2013-08-14 CN CN201380052655.7A patent/CN105051124B/en active Active
- 2013-08-14 US US14/421,559 patent/US9702509B2/en active Active
Non-Patent Citations (1)
Title |
---|
See references of WO2014026764A1 * |
Also Published As
Publication number | Publication date |
---|---|
DE102012016046B3 (en) | 2013-12-24 |
WO2014026764A1 (en) | 2014-02-20 |
CN105051124B (en) | 2017-07-04 |
CN105051124A (en) | 2015-11-11 |
EP2885356B1 (en) | 2017-07-19 |
US9702509B2 (en) | 2017-07-11 |
US20150252951A1 (en) | 2015-09-10 |
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